{"created":"2023-06-20T15:03:23.348208+00:00","id":32586,"links":{},"metadata":{"_buckets":{"deposit":"e2e3c384-9149-4e7e-aa6b-9bffc847d497"},"_deposit":{"created_by":1,"id":"32586","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32586"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032586","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["410228","410231","410230","410226","410229","410223","410232","410224","410225","410222","410233","410227"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Structural Design of Fin for S-520 Type Sounding Rocket"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1980-11","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4_A","bibliographicPageEnd":"1221","bibliographicPageStart":"1207","bibliographicVolumeNumber":"16","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To meet the severe structural requirements imposed on the tail fin of the newly developed S-520 type sounding rocket, two new concepts are adopted. The one is an aluminium honeycomb sandwich plate with carbon fibre reinforeced plastic (CFRP) facing as the structural member, and the other is a glass fibre reinforced plastic (GFRP) cover ablation plate with titanium leading edge to resist the aerodynamic heating. In this paper, research and developmental studies concerning this fin, including the design concept, model tests, aerodynamic heating tests using small solid rocket motor, and statical loading test to failure of the actual fin are presented.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125912000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"日産自動車"},{"subitem_text_value":"日産自動車"},{"subitem_text_value":"日産自動車"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"森, 大吉郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野田, 淳次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋元, 保雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村上, 卓司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"白銀, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野島, 昇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORI, Daikichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ONODA, Junjiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASHIMOTO, Yasuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MURAKAMI, Takuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIROGANE, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ONOJIMA, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"SA0125912.pdf","filesize":[{"value":"756.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125912.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32586/files/SA0125912.pdf"},"version_id":"66121bc0-cc8c-4a57-8593-be87573af75c"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"<論文>S-520ロケット用尾翼の試作","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"<論文>S-520ロケット用尾翼の試作"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32586","relation_version_is_last":true,"title":["<論文>S-520ロケット用尾翼の試作"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:28:39.936434+00:00"}